STC SA00864WI-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00864WI-D This certificate issued to: Garmin International, Inc.

1200 East 151$ Street Olathe, KS 66062 Certifies that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meet's the airworthiness requirement's of Purt 23 of the Federal Aviation Regulations.

Original Product • Type Certificate Number: A3SO Make: Piper Aircraft, Inc Model: PA-32-260 Description of Type Design Change:

Installation of the Garmin GNS 530, 530A, or GPS 500 (GNC 500 Series TAWS Option) in accordance with the installation data and FAA Approved Airplane Flight Manual Supplements (AFMS) listed on the Continuation Sheet (See page 3 of 3).

Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of Application: November 10, 1998 Date Reissued: August 27, 2007 Date of Issuance: March 21, 2000 Date Amended: April 13, 2001; July 25, 2002;

November 22, 2004 FEDERAL AVIATION By Direction of the Administrator (Signature) Robert Murray TOMINSTRATO DAS Administrator DAS-240087-CE Garmin International (Title)

Transfer the ownership of Supplement Type Certificate Number To (Name of trunsferee) (Number and street) (City. Hate and Zip code) From (Name of granter) Print or lype (Address of granter) (Number and street) (City. Hate and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In Ink):

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00364W-D Configuration 1 Installation Data Installation of Garmin GNS 530 or GNS 530A in accordance with Garmin Master Drawing List No. 005-C0097-00, Revision H, dated April 26, 2002, or later FAA Approved revision Configuration 2 Installation Data Installation of the Garmin GPS 500 in accordance with Garmin Master Drawing List No. 005-C0097-00, Revision H, dated April 26, 2002, or later FAA Approved revision.

Configuration 3 Installation Data Installation of the Garmin GNS 530, GNS 530A, or GPS 500 (GNC 500 Series TAWS Option) in accordance with Garmin Master Drawing List No. 005-C0097-00, Revision P, November 17, 2004, or later FAA approved revision.

AFMS FAA Approved Airplane Flight manual Supplement for Piper PA32 with Garmin GNS 530, Drawing No. 190-00181-03, Revision A, signed 04/04/00, or later FAA Approved revision.

AFMS FAA Approved Airplane Flight Manual Supplement for Piper PA32 with Garmin GPS 500, Drawing No. 190-00181-63, Revision A, signed 03/15/01, or later FAA Approved revision.

AFMS FAA Approved Airplane Flight manual Supplement for Piper PA32 with Garmin GNS 530, Drawing No. 190-00181-03, Revision C, signed November, 19, 2004, or later FAA approved revision.

OR FAA Approved Airplane Flight Manual Supplement for Piper PA32 with Garmin GPS 500, Drawing No. 190-00181-63, Revision B, signed November 19, 2004, or later FAA approved revision.